US9868533B2 - Armrest device - Google Patents

Armrest device Download PDF

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Publication number
US9868533B2
US9868533B2 US14/781,409 US201414781409A US9868533B2 US 9868533 B2 US9868533 B2 US 9868533B2 US 201414781409 A US201414781409 A US 201414781409A US 9868533 B2 US9868533 B2 US 9868533B2
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US
United States
Prior art keywords
cushion unit
armrest device
implemented
armrest
comfort
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related, expires
Application number
US14/781,409
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English (en)
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US20160023768A1 (en
Inventor
Christopher Tute
Marc Schmidt
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Recaro Aircraft Seating GmbH and Co KG
Original Assignee
Recaro Aircraft Seating GmbH and Co KG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
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Assigned to RECARO AIRCRAFT SEATING GMBH & CO. KG reassignment RECARO AIRCRAFT SEATING GMBH & CO. KG ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SCHMIDT, MARC, TUTE, Christopher
Publication of US20160023768A1 publication Critical patent/US20160023768A1/en
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0647—Seats characterised by special upholstery or cushioning features
    • B60N2/46—
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/70—Upholstery springs ; Upholstery
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60N—SEATS SPECIALLY ADAPTED FOR VEHICLES; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDED FOR
    • B60N2/00—Seats specially adapted for vehicles; Arrangement or mounting of seats in vehicles
    • B60N2/75—Arm-rests
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
    • B64D11/06—Arrangements of seats, or adaptations or details specially adapted for aircraft seats
    • B64D11/0646—Seats characterised by special features of stationary arms, foot or head rests

Definitions

  • the objective of the invention is, in particular, to provide a generic device with improved characteristics regarding comfort, haptic and variability, in particular as regards a color.
  • the invention proceeds from an armrest device for an aircraft seat, with a cushion unit that is at least substantially implemented by an elastomer and which is provided at least for forming an elastic substrate for an arm support for a passenger.
  • the cushion unit comprises a comfort structure, which is provided for adjustment of an elastic deformability of the cushion unit.
  • a “cushion unit” is herein to be understood, in particular, as a unit of an armrest which forms due to its characteristics a soft, elastically deformable substrate of the armrest, on which a person may rest his arm, the cushion unit being herein implemented preferably in one piece and of one single material, e.g. in particular of an elastomer.
  • the cushion unit has a thickness of maximally 20 millimeters, preferably no more than 10 millimeters and in an especially advantageous embodiment a thickness of less than 5 millimeters.
  • An “elastomer” is herein to mean, in particular, a caoutchouc, a thermoplastic elastomer, e.g. a TPU, or a silicone.
  • An “arm support for a passenger” is to mean, in particular, a zone of an armrest of a seat on which a passenger can rest his arm while sitting on the seat.
  • “Provided” is to mean, in particular, specifically programmed, designed and/or equipped.
  • a “comfort structure” is to mean, in particular, a structure that is introduced into the cushion unit and which has an influence on an elastic deformability due to its design.
  • the structure is herein preferably implemented by one or several pockets or grooves.
  • the pockets or grooves implementing the comfort structure have a depth that corresponds to 80% of the thickness of the cushion unit, advantageously to less than 60% of the thickness of the cushion unit and in an especially advantageous embodiment to 50% of the thickness of the cushion unit.
  • different degrees of deformability i.e. of a hardness of the cushion unit in different zones, are in particular advantageously achievable by differently implementing the comfort structure in different zones of the cushion unit.
  • An “adjusting of an elastic deformability” is herein to mean, in particular, that by a design of the comfort structure an elastic deformability, and hence a hardness of the cushion unit, can be increased or reduced and can thus be set to an elastic deformability that is advantageous and desired for the desired application. In this way a hardness and thus a comfort of the cushion unit can be adapted to different embodiments of the armrest device in a particularly simple and cost-effective fashion.
  • a high level of comfort, haptic and variability of the armrest device is particularly advantageously achievable.
  • a color, a haptic and an elastic characteristic of the cushion unit may be adapted to different seats, in particular to different aircraft seats of different airlines or for different equipment, in a simple and cost-effective fashion.
  • the choice and use of different colors for different armrests is advantageous due to silicone being used, as silicone complies, independently from a specific color, with legal provisions, in particular regarding fire protection in aircraft construction.
  • the cushion unit comprises a support surface and the comfort structure is arranged on a side of the cushion unit that faces away from the support surface.
  • a “support surface” is herein to be understood, in particular, as a surface of the cushion unit which is arranged on a side facing away from a frame of an armrest on which the cushion unit is arranged, and which forms a surface provided for a person sitting on the seat with the armrest to rest an arm on.
  • the comfort structure can be arranged in an especially advantageous and simple fashion.
  • comfort structure is implemented by a filigree structure.
  • a “filigree structure” is to mean, in particular, a structure of pockets adjacent to each other or of one or several contiguous grooves, which extend over an entire surface of the comfort structure. Thus the comfort structure can be easily implemented.
  • the comfort structure is implemented as a planar polygonal grid structure.
  • a “planar polygonal grid structure” is to mean, in particular, a structure of pockets that are arranged one beside the other, each of which has a polygonal shape.
  • the planar polygonal grid structure is, for example, embodied as an arrangement of rectangular, square or triangular pockets which are adjacent to each other.
  • the planar polygonal grid structure is embodied as a honeycomb structure formed of preferably equilateral, hexagonal pockets that are adjacent to each other.
  • the planar polygonal grid structure implemented as a honeycomb structure preferably has a width of 5 mm and a wall thickness of 1.5 mm.
  • the cushion unit is implemented at least substantially by a silicone.
  • at least substantially is herein to be understood, in particular, that the cushion unit is embodied as a silicone by at least 60%, preferably by 90% and in an especially advantageous implementation entirely.
  • a “silicone” is herein to be understood, in particular, a silicone elastomer, which in particular forms a mass having a rubber-like elasticity.
  • the armrest device comprises a coating, which at least partially encompasses the cushion unit for the purpose of protection.
  • a “coating” is to mean, in particular, a layer applied onto the armrest device, which is provided at least for improving haptic characteristics of the armrest device.
  • the coating is fixedly connected to the cushion unit by substance-to-substance bond, by form-lock and/or by means of an adhesive bond.
  • the coating is preferably embodied by a thin layer of varnish, which is applied onto the cushion unit embodied as a silicone by a suitable method, while entering a substance-to-substance bond with the cushion unit and/or while being adhesively connected to the cushion unit.
  • the coating is embodied as a cover made of a fabric, a leather or another cover that is deemed expedient by the person skilled in the art and is manufactured naturally or artificially, which cover is fitted over the cushion unit implemented by silicone.
  • “at least partially encompassing” is to mean, in particular, that the coating completely covers the cushion unit at least on the support surface formed by the cushion unit and on surfaces which in a fully assembled state can be seen and/or touched by a passenger.
  • the cushion unit is herein preferably completely covered by the coating.
  • the armrest device comprises an inlay, which is at least substantially encompassed by the cushion unit that is at least substantially implemented by a silicone.
  • An “inlay” is herein to mean, in particular, a carrier structure, which is embodied, in particular, in an early manufacturing stage of the armrest device as a separate individual element, which is fixedly connected to the cushion unit during one manufacturing step.
  • the inlay is herein embodied as a carrier structure for the cushion unit and preferably comprises connection elements, by means of which the armrest device can be fixedly connected to a frame of an armrest.
  • the inlay is covered by the cushion unit to at least 50%, preferably at least over an entire side that faces the support surface of the cushion unit.
  • the inlay is herein preferably connected to the cushion unit by means of a form-fit, adhesive and/or substance-to-substance connection.
  • the inlay is at least substantially implemented by a high-temperature resistant material.
  • a “high-temperature resistant material” is herein to be understood, in particular, a material that is dimensionally stable up to a temperature of 180° C. and in an especially advantageous embodiment up to a temperature of 280° C.
  • the high-temperature resistant material is preferentially implemented by a high-temperature resistant plastic, e.g. a polyamide or a polycarbonate.
  • the high-temperature resistant material is implemented by a metal, e.g. aluminum, or by another natural or artificial material that is dimensionally stable up to a temperature of 180° C. or particularly advantageously up to a temperature of 280° C.
  • the inlay can be embodied in a particularly advantageous fashion, in particular for manufacturing the armrest device from a silicone.
  • the inlay is implemented at least substantially by a fiber-reinforced composite material.
  • a fiber-reinforced composite is herein to be understood, in particular, that the inlay is implemented by a fiber-reinforced composite preferably by 60%, especially advantageously by 90% and in a particularly advantageous embodiment entirely.
  • a “fiber-reinforced composite” is to mean, in particular, a multi-phase material comprising at least two main components, and comprising at least one embedding matrix as well as reinforcing fibers.
  • the embedding matrix may preferably be embodied as a plastic, a resin and/or a further material that is deemed expedient by the person having ordinary skill in the art, and the fibers can be implemented by plastic fibers, glass fibers, carbon fibers, natural fibers and/or other fibers that are deemed expedient by the person having ordinary skill in the art.
  • the inlay can in particular be implemented with a favorable stiffness-to-weight ratio.
  • the seat is herein preferably embodied as an aircraft seat for being mounted in an aircraft, principally it is, however, also conceivable that the seat is embodied as a vehicle seat, as an office chair, an armchair or as another seat that is deemed expedient by the person having ordinary skill in the art.
  • the armrest device according to the invention is herein not to be limited to the application and implementation form described above.
  • the armrest device according to the invention may comprise, for implementing a functionality herein described, a number of respective elements, structural components and units that differs from a number herein mentioned.
  • FIG. 1 a section view through an armrest device according to the invention in a first exemplary embodiment on a base plate of the armrest,
  • FIG. 2 the armrest device and the base plate in a schematic exploded view
  • FIG. 3 an armrest device according to the invention in a second exemplary embodiment
  • FIG. 4 the armrest device in the second exemplary embodiment in an exploded view
  • FIG. 5 a schematic depiction of the armrest device in the second exemplary embodiment with a section thereof.
  • FIGS. 1 and 2 show a first exemplary embodiment of an armrest device 20 a according to the invention.
  • the armrest device 20 a is embodied as part of a seat that is not shown in detail.
  • the seat is herein implemented as an aircraft seat.
  • the seat that is implemented as an aircraft seat comprises a backrest for supporting a back of a passenger.
  • the seat further comprises a seat bottom, which forms a seat surface for the passenger.
  • the seat comprises a mounting unit, at which the backrest and the seat bottom are arranged.
  • the seat implemented as an aircraft seat is furthermore mounted on a floor of a passenger cabin by means of the mounting unit.
  • the seat comprises laterally to the seat surfaces respectively one armrest 22 a , which is provided to form an arm support for a passenger.
  • the armrests 22 a delimit the seat bottom laterally and supply the passenger with an opportunity of resting his arms while sitting.
  • the armrests 22 a herein each comprise a frame (not shown in detail), which extends from the seat bottom in a direction away from the floor on which the aircraft seat is mounted.
  • the armrest device 20 a is part of the only partially shown armrest 22 a and is fastened to the frame of the armrest 22 a to form a support surface 14 a for an arm of a person sitting on the seat.
  • the frame of the armrest 22 a comprises a base plate 24 a , which forms a base surface of the armrest 22 a .
  • a base surface of the armrest 22 a is herein embodied approximately rectangular, having a long side and a short side.
  • the long side of the base surface of the armrest 22 a is herein, in an assembled state, oriented parallel to a seat direction. It is herein conceivable that the base surface of the armrest 22 a has differing widths over its longer side, i.e. along its longitudinal extension. It is herein principally conceivable that the base surface of the armrest 22 a is domed in its longitudinal extension and/or in its extension over a width.
  • an end of the base plate 24 a that faces towards the backrest is designated as a rear end
  • an end of the base plate 24 a facing away from the backrest is designated as a front end 26 a
  • a side facing towards the seat bottom is designated as an inner side 28 a
  • a side facing away from the seat bottom is designated as an outer side 30 a of the base plate 24 a .
  • the base plate 24 a comprises at its underside 32 a , which faces towards the floor of the passenger cabin, a plurality of fastening domes 34 a , via which the base plate 24 a is fixedly connected to the frame of the armrest 22 a by means of a screw connection.
  • the armrest device 20 a is in an assembled state mounted on the base plate 24 a of the frame of the armrest 22 a .
  • structural elements, units and/or elements of which there are more than one, are respectively given only one reference numeral in FIGS. 1 to 5 .
  • the armrest device 20 a comprises a cushion unit 10 a .
  • the cushion unit 10 a is provided to form an elastic substrate for the arm support of the passenger.
  • the cushion unit 10 a has a shape of the armrest 22 a .
  • the cushion unit 10 a has a thickness of four millimeters.
  • the cushion unit 10 a extends over the entire base surface of the base plate 24 a of the armrest 22 a .
  • the cushion unit 10 a engages around the base plate 24 a , whereby the cushion unit 10 a entirely encompasses the base plate 24 a in a zone that can be touched by a passenger.
  • the cushion unit 10 a comprises an interior side 36 a , which faces in the assembled state towards the base plate 24 a and with which the cushion unit 10 a lies upon the base plate 24 a .
  • An exterior side 38 a of the cushion unit 10 a is arranged on the side of the cushion unit 10 a opposite the interior side 36 a and delimits the cushion unit 10 a towards the outside.
  • the exterior side 38 a of the cushion unit 10 a is herein embodied substantially planar. Principally it is also conceivable that the exterior side 38 a has a pattern of bulges and/or hollows for modifying a haptic.
  • a surface of the exterior side 38 a of the cushion unit 10 a that extends parallel to the base plate 24 a is embodied as a support surface 14 a .
  • the cushion unit 10 a is implemented by a silicone.
  • the cushion unit 10 a is completely implemented by a silicone.
  • the silicone is herein embodied as a silicone elastomer.
  • the silicone which is embodied as a silicone elastomer, has a Shore hardness of 50 Shore A. Principally it is also conceivable that the silicone has another Shore hardness, e.g. a Shore hardness of 40 Shore A or 70 Shore A.
  • the cushion unit 10 a implemented by silicone herein has a solid structure and an elastic deformability. By a force impact from the outside, e.g. by laying an arm on, the cushion unit 10 a implemented by silicone is elastically deformed. When the force applied from outside has been released, the cushion unit 10 a reverts from its elastically deflected state into its normal state.
  • the cushion unit 10 a For adjusting an elastic deformability, the cushion unit 10 a comprises a comfort structure 12 a .
  • the comfort structure 12 a is herein implemented by a filigree structure.
  • the comfort structure 12 a is implemented as a structure of pockets 40 a that are adjacent to each other.
  • an elastic deformability of the cushion unit 10 a is increased, as in case of a load the material of the cushion unit 10 a can spread into the hollow spaces formed by the comfort structure 12 a .
  • the elastic deformability can be easily adjusted for different armrest devices that have to fulfill, for example, different comfort requirements and for this need to have different elastic deformabilities.
  • the comfort structure 12 a is arranged on a side that faces away from the support surface 14 a of the cushion unit 10 a , namely on the underside 32 a of the cushion unit 10 a .
  • the comfort structure 12 a is preferably not visible from the outside for a passenger.
  • the comfort structure 12 a is embodied as a planar polygonal grid structure.
  • the comfort structure 12 a forms honeycomb-shaped pockets 40 a that are adjacent to each other and implement the entire comfort structure 12 a .
  • the comfort structure 12 a herein extends over the entire underside 32 a of the cushion unit 10 a . It is herein also conceivable that regions of the underside 32 a of the cushion unit 10 a do not comprise a comfort structure 12 a and/or that the comfort structure 12 a has in partial regions of the underside 32 a of the cushion unit 10 a a shape and/or size different than in other partial regions, as a result of which an elastic deformability can be adjusted differently for differing partial regions of the cushion unit 10 a .
  • the pockets 40 a herein have a depth of two millimeters, by which the pockets 40 a extend into the cushion unit 10 a.
  • the armrest device 20 a comprises a coating 16 a , which encompasses the cushion unit 10 a .
  • the coating 16 a encompasses the cushion unit 10 a completely at its exterior side 38 a and its interior side. Principally it is also conceivable that the coating 16 a completely encompasses the cushion unit 10 a only on an exterior side 38 a , which can be touched and/or seen by a passenger.
  • the coating 16 a is herein embodied as a silicone varnish.
  • the silicone varnish is herein applied onto the cushion unit 10 a in a manufacturing process of the armrest device 20 a and in this enters into a substance-to-substance bond with the cushion unit 10 a .
  • the coating 16 a is embodied of a thin material that is fitted onto the cushion unit 10 a , e.g. a fabric or leather.
  • the coating 16 a is connected to the cushion unit 10 a in a form-lock and/or by an adhesive bond.
  • the armrest device 20 a For the connection of the armrest device 20 a to the base plate 24 a of the armrest 22 a , the armrest device 20 a comprises a form-lock unit.
  • the form-lock unit comprises a plurality of form-lock elements 42 a , 44 a , 46 a , which in an assembled state fixedly connect the armrest device 20 a to the base plate 24 a .
  • the form-lock elements 42 a , 44 a , 46 a of the armrest device 20 a are herein embodied in a one-part implementation with the cushion unit 10 a that is implemented from silicone.
  • one form-lock element 42 a is arranged at an inner side, one form-lock element 44 a at an outer side, one form-lock element 46 a at a front end and one form-lock element at a rear end of the cushion unit 10 a .
  • the form-lock elements that are embodied correspondingly to the form-lock elements 42 a , 44 a , 46 a of the armrest device 20 a are implemented by the respective sides 28 a , 30 a and by ends 26 a of the base plate 24 a , which are in an assembled state encompassed by the cushion unit 10 a .
  • the form-lock elements 42 a , 44 a , 46 a of the armrest device 20 a engage around the corresponding form-lock elements implemented by the ends 26 a and sides 28 a , 30 a of the base plate 24 a , thereby fixedly connecting the cushion unit 10 a and thus the armrest device 20 a to the base plate 24 a of the armrest 22 a .
  • the cushion unit 10 a that is implemented of silicone is during assembly elastically expanded to such an extent that the form-lock elements 42 a , 44 a , 46 a of the armrest device 20 a engage into the form-lock elements of the base plate 24 a , the cushion unit 10 a thus completely encompassing the base plate 24 a .
  • the cushion unit 10 a contracts and is thus pressed into the form-lock elements of the base plate 24 a together with the form-lock elements 42 a , 44 a , 46 a , as a result of which a holding force is generated between the form-lock elements 42 a , 44 a , 46 a of the armrest device 20 a and the base plate 24 a .
  • the armrest device 20 a is fixedly and securely connected to the base plate 24 a .
  • a securing element e.g. a screw, connects the armrest device 20 a to the base plate 24 a , in addition to the form-lock elements 42 a , 44 a , 46 a.
  • FIGS. 3 to 5 a further exemplary embodiment of the invention is shown.
  • the following description and the drawings are substantially limited to the differences between the exemplary embodiments, wherein regarding identically designated structural elements, in particular regarding structural elements with the same reference numerals, principally the drawings and/or the description of the other exemplary embodiment in particular of FIGS. 1 and 2 may be referred to.
  • the letter a is put after the reference numerals of the exemplary embodiment in FIGS. 1 and 2 .
  • the letter a has been replaced by the letter b.
  • FIGS. 3 to 5 show a second exemplary embodiment of an armrest device 20 b according to the invention.
  • the armrest device 20 b is embodied as part of a seat that is not shown in detail.
  • the armrest device 20 b is part of an only partially shown armrest 22 b and is fastened to a frame of the armrest 22 b to form a support surface for a person sitting on the seat.
  • the frame of the armrest 22 b comprises a base plate (not shown in detail), which forms a base surface of the armrest 22 b.
  • the armrest device 20 b comprises a cushion unit 10 b .
  • the cushion unit 10 b is provided to form an elastic substrate for the arm support of the passenger.
  • the cushion unit 10 b has a shape of the armrest 22 b .
  • the cushion unit 10 b extends over the entire base surface of the base plate of the armrest 22 b .
  • the cushion unit 10 b comprises a comfort structure 12 b .
  • the comfort structure 12 b is implemented as a structure of pockets that are adjacent to each other.
  • the comfort structure 12 b is implemented as a planar polygonal grid structure.
  • the comfort structure 12 b forms rectangular pockets that are adjacent to each other and implement the entire comfort structure 12 b .
  • the comfort structure 12 b extends over an entire underside of the cushion unit 10 b.
  • the armrest device 20 b comprises an inlay 18 b .
  • the inlay 18 b is partially encompassed by the cushion unit 10 b that is implemented of silicone.
  • the inlay 18 b substantially has the shape of the base plate of the armrest 22 b .
  • the inlay 18 b comprises a frame 48 b , which delimits the inlay 18 b at an inner side, an outer side, a front end and at a rear end.
  • the frame 48 b of the inlay 18 b is herein embodied of solid material.
  • the frame 48 b completely encompasses a middle region of the inlay 18 b .
  • the middle region of the inlay 18 b is herein implemented by a lattice structure 50 b .
  • the lattice structure 50 b is embodied correspondingly to the comfort structure 12 b of the cushion unit 10 b .
  • the lattice structure 50 b is implemented by rectangles that are adjacent to each other.
  • the inlay 18 b is in a pre-assembled state connected to the cushion unit 10 b in a form-lock and a substance-to-substance bond.
  • the inlay 18 b is then, preferably in a hardened state, encompassed by the cushion unit 10 b implemented by silicone in an injection-molding process.
  • the comfort structure 12 b of the cushion unit 10 b is herein achieved by injecting through the lattice structure 50 b of the inlay 18 b .
  • the cushion unit 10 b connects during manufacturing to the inlay 18 b of the armrest device 20 b by adhesive bond, substance-to-substance bond and/or by form-lock.
  • the inlay 18 b is embodied of a high-temperature resistant material.
  • the inlay 18 b is herein made of a fiber-reinforced composite, which is implemented by an embedding matrix and glass fibers embedded in the matrix.
  • the inlay 18 b which is implemented of the high-temperature resistant fiber-reinforced composite, is dimensionally stable up to temperatures of 280° C., as a result of which a tempering process of the cushion unit 10 b that is implemented of silicone can be carried out with the inlay 18 b located in the cushion unit 10 b without deformation of the inlay 18 b.
  • the inlay 18 b comprises a plurality of form-lock elements 52 b .
  • the form-lock elements 52 b are herein arranged at an underside of the inlay 18 b , which in an assembled state faces towards the base plate.
  • the form-lock elements 52 b are embodied in a one-part implementation with the inlay 18 b .
  • the form-lock elements 52 b are herein embodied as latch hook, which in the assembled state latch into latch elements (not shown in detail) of the base plate, fixedly connecting the armrest device 20 b to the base plate.
  • the armrest device 20 b is fixedly connected to the base plate by means of a different connection method that is deemed expedient by the person having ordinary skill in the art, e.g. by an adhesive bond or by another form-lock and/or force-lock connection.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Seats For Vehicles (AREA)
US14/781,409 2013-04-04 2014-03-27 Armrest device Expired - Fee Related US9868533B2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DE102013103382.2 2013-04-04
DE102013103382.2A DE102013103382A1 (de) 2013-04-04 2013-04-04 Armlehnenvorrichtung
DE102013103382 2013-04-04
PCT/EP2014/056142 WO2014161765A1 (de) 2013-04-04 2014-03-27 Armlehnenvorrichtung

Publications (2)

Publication Number Publication Date
US20160023768A1 US20160023768A1 (en) 2016-01-28
US9868533B2 true US9868533B2 (en) 2018-01-16

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Family Applications (1)

Application Number Title Priority Date Filing Date
US14/781,409 Expired - Fee Related US9868533B2 (en) 2013-04-04 2014-03-27 Armrest device

Country Status (5)

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US (1) US9868533B2 (de)
EP (1) EP2981467B1 (de)
CN (1) CN105263803A (de)
DE (1) DE102013103382A1 (de)
WO (1) WO2014161765A1 (de)

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DE202015101784U1 (de) * 2015-04-13 2016-07-14 Zim Flugsitz Gmbh Armlehne zur Anbringung an einem Flugzeugsitz
US9994137B2 (en) * 2016-02-16 2018-06-12 Ford Global Technologies, Llc Deformable armrest having a patterned array of channels
US10286821B1 (en) * 2017-10-24 2019-05-14 Ford Global Technologies, Llc Armrest core, armrest incorporating that armrest core and method of manufacturing that armrest assembly
GB2572159A (en) * 2018-03-20 2019-09-25 Mirus Aircraft Seating Ltd Storage pocket
WO2022076567A1 (en) * 2020-10-07 2022-04-14 Shanghai Yanfeng Jinqiao Automotive Trim Systems Co. Ltd. Vehicle interior component
JP7510455B2 (ja) * 2022-03-23 2024-07-03 森六テクノロジー株式会社 車両用内装構造
US20230406181A1 (en) * 2022-05-27 2023-12-21 Lear Corporation Pivoting armrest for seat

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CN105263803A (zh) 2016-01-20
DE102013103382A1 (de) 2014-10-09
US20160023768A1 (en) 2016-01-28
WO2014161765A1 (de) 2014-10-09
EP2981467A1 (de) 2016-02-10

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